Iceland

The twin engine aircraft departed Reykjavik Airport on a schedule flight to Selfoss, Southern Region. While flying under VFR mode in IMC conditions, the pilot failed to realize his altitude was too low when the aircraft struck the slope of Mt Geitarhilđ located near Lake Kleif, about 20 km south of Reykjavik. The aircraft was destroyed by impact forces and a post crash fire and the pilot, sole on board, was killed.

The crew was repatriating the aircraft from Kinshasa, Zaire, to the US. On the leg from Biggin Hill to Reykjavik, while approaching the Icelandic coast, the left engine failed. The crew declared an emergency and was cleared to divert to Vestmannaeyjar Airport. While circling for landing, the right engine failed as well. The crew lost control of the airplane that crashed in the sea few km offshore. Both occupants were killed.

While approaching Iceland on a ferry flight from Frobisher Bay, the crew declared an emergency due to fuel shortage and requested the permission to divert to Keflavik Airport. On final approach to runway 29, both engines failed simultaneously. The aircraft stalled and crashed on a road located 1,500 meters short of runway. Both pilots were injured and the aircraft was destroyed.

The CASA 212 was bought by Geoterrex in 1983 and registered in Canada in 1985. The plane had been extensively modified for aerial survey work. These modifications consisted of two probes mounted on the fuselage above the cockpit and extending 10 feet in front of the aircraft nose, a l6-foot tail boom, and two wing tip pylons. The probes, pylons, and tail boom served to support a wire loop antenna which ran around the aircraft. In July 1988 the plane was prepared for a ferry flight across the Atlantic to Nantes, France. For the purposes of this ferry trip, the survey loop antenna and the wing tip pylons had been removed and stowed in the main cabin area. For this configuration a special ferry permit was necessary, but the company did not apply for one. On July 31, 1988 the aircraft departed Ottawa and arrived at Goose Bay later that day. On 2 August 1988, the aircraft departed Goose Bay at 09:05 UTC and arrived at Narsarsuaq, Greenland at 12:50 UTC. The aircraft was refuelled and departed one hour later at 13:50 UTC for Reykjavik, Iceland, at a planned altitude of FL130. Although the pilot’s instrument rating had expired and the co-pilot did not possess one, the crew filed an IFR flight plan to Reykjavik. The weight of the aircraft was about 3,000 pounds above the maximum authorized takeoff weight on takeoff from Narsarsuaq. At Reykjavik, the crew flew an ILS approach to runway 20. During the approach, the flaps were set at approximately 25 degrees, 15 degrees above the approved maximum of 10 degrees. Approximately one-half mile from the runway threshold, the aircraft entered a steep turn to the right, and the nose of the aircraft dropped sharply. The aircraft continued to turn to the right through 270 degrees and descended rapidly until it struck the ground approximately 900 feet short of the runway threshold. The aircraft burst into flames shortly after impact.

Recently purchased by the Spanish operator Drenair, the aircraft departed West Palm Beach, Florida, on a delivery flight to Spain, carrying four passengers and two pilots. After a fuel stop in Bedford, Massachusetts, and Goose Bay, Newfoundland, the aircraft continued to Keflavik, Iceland. While approaching Keflavik, the crew declared an emergency due to fuel exhaustion, informed ATC about his position and ditched the aircraft approximately 70 km southwest of Keflavik. All six occupants were quickly rescued by the crew of a helicopter while the aircraft sank and was lost.

While approaching Isafjörđur Airport, the pilot encountered poor visibility due to the night and poor weather conditions. While trying to locate the airport, he lost control of the airplane that crashed in the sea about six km offshore. The aircraft sank and was lost and the pilot, sole on board, was killed.

Shortly after takeoff from Höfn-Hornafjörður Airport runway 36, the twin engine aircraft crashed in unknown circumstances in a river located about 200 meters from the runway end. All occupants were rescued while the aircraft was written off.

While descending to Egilsstađir Airport, the pilot encountered poor weather conditions with limited visibility due to low clouds. While flying under VFR mode, the twin engine airplane struck the slope of Mt Smjörfjöll (1,251 meters high) located few km from the destination. All three occupants were killed.

While taxiing at Keflavik Airport, the left main gear collapsed. The airplane sank on its belly, causing the propellers of both left engine to struck the ground as well. A fuel tank was punctured and a fire erupted. All 17 occupants were able to evacuate safely while the aircraft was destroyed by fire.

After touchdown, the airplane went out of control, veered off runway and collided with a hangar. There were no casualties but the aircraft was damaged beyond repair.